Year |
Citation |
Score |
2016 |
Pirau S, Liberi B, Barbely N, Komerath N. Aerodynamic load maps of bluff bodies: Measurement and diagnostics Journal of Mechanical Science and Technology. 30: 3961-3967. DOI: 10.1007/S12206-016-0808-Z |
0.32 |
|
2015 |
Raghav V, Komerath N. Advance ratio effects on the flow structure and unsteadiness of the dynamic-stall vortex of a rotating blade in steady forward flight Physics of Fluids. 27: 27101. DOI: 10.1063/1.4906803 |
0.349 |
|
2014 |
Gregory JW, Disotell KJ, Peng D, Juliano TJ, Crafton J, Komerath NM. Inverse methods for deblurring pressure-sensitive paint images of rotating surfaces Aiaa Journal. 52: 2045-2061. DOI: 10.2514/1.J052793 |
0.331 |
|
2014 |
Disotell KJ, Peng D, Juliano TJ, Gregory JW, Crafton JW, Komerath NM. Single-Shot temperature- And pressure-Sensitive paint measurements on an unsteady helicopter blade Experiments in Fluids. 55. DOI: 10.1007/S00348-014-1671-2 |
0.378 |
|
2014 |
Raghav V, Komerath N. Velocity measurements on a retreating blade in dynamic stall Experiments in Fluids. 55: 1669. DOI: 10.1007/S00348-014-1669-9 |
0.382 |
|
2013 |
Raghav V, Komerath N. An Exploration of Radial Flow on a Rotating Blade in Retreating Blade Stall Journal of the American Helicopter Society. 58: 1-10. DOI: 10.4050/Jahs.58.022005 |
0.371 |
|
2013 |
Raghav V, Komerath N. Instability of the radial flow over a rotating disk in a separated edgewise stream Physics of Fluids. 25: 111701. DOI: 10.1063/1.4833435 |
0.332 |
|
2013 |
Sharma S, Raghav V, Komerath N, Smith M. Wall effect on fluid–structure interactions of a tethered bluff body Physics Letters A. 377: 2079-2082. DOI: 10.1016/J.Physleta.2013.06.002 |
0.338 |
|
2013 |
Raghav V, Shenoy R, Smith M, Komerath N. Investigation of drag and wake turbulence of a rotor hub Aerospace Science and Technology. 28: 164-175. DOI: 10.1016/J.Ast.2012.10.012 |
0.404 |
|
2012 |
Komerath NM, Pant R, Kar A. An architecture using lighter-than-air platforms for retail power beaming and communications Journal of Low Power Electronics. 8: 261-269. DOI: 10.1166/Jolpe.2012.1190 |
0.32 |
|
2012 |
Komerath N, Kar A. Retail beamed power using millimeter waves: Survey Acm Journal On Emerging Technologies in Computing Systems. 8: 18. DOI: 10.1145/2287696.2287701 |
0.307 |
|
2011 |
Komerath NM, Smith MJ, Tung C. A review of rotor wake physics and modeling Journal of the American Helicopter Society. 56. DOI: 10.4050/Jahs.56.022006 |
0.324 |
|
2011 |
Komerath NM, Komerath PP. Terrestrial micro renewable energy applications of space technology Physics Procedia. 20: 255-269. DOI: 10.1016/J.Phpro.2011.08.024 |
0.311 |
|
2007 |
Wanis SS, Rangedera T, Komerath NM. Particle-particle interaction in electromagnetic fields for force-field tailoring Aip Conference Proceedings. 880: 177-184. DOI: 10.1063/1.2437454 |
0.747 |
|
2006 |
Gregory JW, Sullivan JP, Wanis SS, Komerath NM. Pressure-sensitive paint as a distributed optical microphone array. The Journal of the Acoustical Society of America. 119: 251-61. PMID 16454281 DOI: 10.1121/1.2140935 |
0.737 |
|
2006 |
Komerath N, Satyshur P, Rangedera T, Wanis S. System Design of Large Space Structures Using Tailored Force Fields Space. DOI: 10.2514/6.2006-7323 |
0.754 |
|
2006 |
Boechler N, Hameer S, Wanis S, Komerath N. An evolutionary model for space solar power Aip Conference Proceedings. 813: 1189-1196. DOI: 10.1063/1.2169301 |
0.735 |
|
2006 |
Wanis SS, Komerath NM. Validation of tailored force fields concept for use in space-based construction Aip Conference Proceedings. 813: 1170-1177. DOI: 10.1063/1.2169299 |
0.765 |
|
2006 |
Vasilescu R, Ganesh B, Dancila DS, Komerath NM, Sankar LN. Geometry tip cap effects on formation and near wake evolution of the rotor tip vortices Collection of Technical Papers - 36th Aiaa Fluid Dynamics Conference. 2: 1306-1319. |
0.606 |
|
2005 |
Vanmali R, Tomlinson B, Li B, Wanis S, Komerath N. Engineering a Space Based Construction Robot Sae Transactions. 114: 1375-1382. DOI: 10.4271/2005-01-3406 |
0.762 |
|
2005 |
Vanmali R, Li B, Tomlinson B, Zaidi W, Wanis S, Komerath N. Conceptual Design of a Multipurpose Robotic Craft for Space Based Construction Space. DOI: 10.2514/6.2005-6733 |
0.755 |
|
2004 |
Wanis SS, Komerath NM. Use of Radiation Pressure for Space-Based Construction Engineering Construction and Operations in Challenging Environments Earth and Space 2004: Proceedings of the Ninth Biennial Asce Aerospace Division International Conference. 317-324. |
0.763 |
|
1999 |
Wanis S, Sercovich AH, Komerath NM. Acoustic shaping in microgravity: Higher order surface shapes 37th Aerospace Sciences Meeting and Exhibit. |
0.768 |
|
1998 |
Affes H, Xiao Z, Conlisk AT, Kim JM, Komerath NM. Model for rotor tip vortex-airframe interaction part 3: Viscous flow on airframe Aiaa Journal. 36: 409-415. DOI: 10.2514/2.378 |
0.358 |
|
1998 |
Reddy UC, Matos CM, Mahalingam R, Funk RB, Komerath NM. Velocity measurement in a rotor wake interacting with a fixed wing 36th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.303 |
|
1997 |
Darden LA, Komerath N. Aircraft control using stagnation point displacement Sae Technical Papers. DOI: 10.4271/975590 |
0.342 |
|
1997 |
Komerath NM, Ames RG, Magill JC. Expanding the role of the wind-driven manipulator Sae Technical Papers. DOI: 10.4271/975589 |
0.362 |
|
1997 |
Mahalingam R, Funk RB, Komerath NM. Low speed canard-tip-vortex airfoil interaction Sae Technical Papers. DOI: 10.4271/971469 |
0.383 |
|
1996 |
Magill JC, Darden LA, Komerath NM. Flow visualization during multiple-axis motions using a wind-driven manipulator Journal of Aircraft. 33: 163-170. DOI: 10.2514/3.46917 |
0.35 |
|
1996 |
Hubner JP, Komerath NM. Counter-rotating structures over a delta wing Aiaa Journal. 34: 1958-1960. DOI: 10.2514/3.13337 |
0.302 |
|
1995 |
Foley SM, Funk RB, Fawcett PA, Komerath NM. Rotor-wake-induced flow separation on a lifting surface Journal of the American Helicopter Society. 40: 24-27. DOI: 10.4050/Jahs.40.24 |
0.351 |
|
1995 |
Lal MK, Liou SG, Pierce GA, Komerath NM. Correlation of Unsteady Pressure and Inflow Velocity Fields of a Pitching Rotor Blade Journal of Aircraft. 32: 520-528. DOI: 10.2514/3.46751 |
0.382 |
|
1995 |
Hubner JP, Komerath NM. Spectral Mapping of Quasiperiodic Structures in a Vortex Flow Journal of Aircraft. 32: 493-500. DOI: 10.2514/3.46747 |
0.357 |
|
1995 |
Kim JM, Komerath NM. Summary of the interaction of a rotor wake with a circular cylinder Aiaa Journal. 33: 470-478. DOI: 10.2514/3.12600 |
0.36 |
|
1994 |
Kim JM, Komerath NM, Liou SG. Vorticity concentration at the edge of the inboard vortex sheet Journal of the American Helicopter Society. 39: 30-34. DOI: 10.4050/Jahs.39.30 |
0.374 |
|
1994 |
Liou SG, Komerath NM, Lal MK. Measurement around a rotor blade excited in pitch, Part 1: Dynamic flow Journal of the American Helicopter Society. 39: 3-12. DOI: 10.4050/Jahs.39.2.3 |
0.331 |
|
1994 |
Lal MK, Liou SG, Pierce GA, Komerath NM. Measurement around a rotor blade excited in pitch, Part 2: Unsteady surface pressure Journal of the American Helicopter Society. 39: 13-20. DOI: 10.4050/Jahs.39.13 |
0.37 |
|
1993 |
Affes H, Conlisk AT, Kim JM, Komerath NM. Model for rotor tip vortex-airframe interaction. II - Comparison with experiment Aiaa Journal. 31: 2274-2282. DOI: 10.2514/3.11925 |
0.336 |
|
1993 |
Komerath NM, Kim JM, Liou SG. Rotor wake interaction with separated flow Mathematical and Computer Modelling. 18: 73-87. DOI: 10.1016/0895-7177(93)90105-8 |
0.383 |
|
1992 |
Komerath NM, Liou SG, Schwartz RJ, Kim JM. Flow over a twin-tailed aircraft at angle of attack. II - Temporal characteristics Journal of Aircraft. 29: 413-420. DOI: 10.2514/3.46177 |
0.351 |
|
1991 |
Komerath NM, Mavris DM, Liou SG. Prediction of unsteady pressure and velocity over a rotorcraft in forward flight Journal of Aircraft. 28: 509-516. DOI: 10.2514/3.46056 |
0.409 |
|
1990 |
Brand AG, McMahon HM, Komerath NM. Correlations of Rotor Wake/Airframe Interaction Measurements with Flow Visualization Data Journal of the American Helicopter Society. 35: 4-15. DOI: 10.4050/Jahs.35.4 |
0.397 |
|
1990 |
Liou SG, Komerath NM, Mcmahon HM. Velocity field of a cylinder in the wake of a rotor in forward flight Journal of Aircraft. 27: 804-809. DOI: 10.2514/3.45940 |
0.411 |
|
1990 |
Liou SG, Komerath NM, McMahon HM. Measurement of the interaction between a rotor tip vortex and a cylinder Aiaa Journal. 28: 975-981. DOI: 10.2514/3.25153 |
0.384 |
|
1989 |
Mavris DN, Komerath NM, McMahon HM. Prediction of aerodynamic rotor-airframe interactions in forward flight Journal of the American Helicopter Society. 34: 37-46. DOI: 10.4050/Jahs.34.37 |
0.367 |
|
1989 |
Brand A, Komerath N, Mcmahon H. Results from laser sheet visualization of a periodic rotor wake Journal of Aircraft. 26: 438-443. DOI: 10.2514/3.45782 |
0.37 |
|
1989 |
Liou SG, Komerath NM, McMahon HM. Velocity measurements of airframe effects on a rotor in low-speed forward flight Journal of Aircraft. 26: 340-348. DOI: 10.2514/3.45766 |
0.387 |
|
1989 |
Brand AG, McMahon HM, Komerath NM. Surface pressure measurements on a body subject to vortex wake interaction Aiaa Journal. 27: 569-574. DOI: 10.2514/3.10147 |
0.37 |
|
1988 |
Thompson TL, Komerath NM, Gray RB. Visualization and measurement of the tip vortex core of a rotor blade in hover Journal of Aircraft. 25: 1113-1121. DOI: 10.2514/3.45710 |
0.374 |
|
1988 |
Brand AG, Komerath NM, McMahon HM. Laser sheet technique for visualizing a periodic rotor wake Journal of Aircraft. 25: 667-669. DOI: 10.2514/3.45640 |
0.364 |
|
1985 |
Komerath NM, Hegde UG, Strahle WC. TURBULENT STATIC PRESSURE FLUCTUATIONS AWAY FROM FLOW BOUNDARIES Aiaa Journal. 23: 1320-1326. DOI: 10.2514/3.9087 |
0.671 |
|
1985 |
Chandran SBS, Komerath NM, Grissom WM, Jagoda JI, Strahle WC. Time resolved thermometry by simultaneous thermocouple and rayleigh scattering measurements in a turbulent flame Combustion Science and Technology. 44: 47-60. DOI: 10.1080/00102208508960292 |
0.639 |
|
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